Performance Evaluation of Stewart-Gough Flight Simulator Based on <inline-formula><math display="inline"><semantics><mrow><msub><mi mathvariant="bold-script">L</mi><mn>1</mn></msub></mrow></semantics></math></inline-formula> Adaptive Control
In the design of the six degrees of freedom (6-DOF) flight simulation system, the unmodeled dynamic, transient performance and steady-state performance of the system are generally concerned. Considering that the model of flight simulation system is highly nonlinear and requires high response speed a...
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| Principais autores: | , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
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MDPI AG
2021-04-01
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| Colecção: | Applied Sciences |
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| Acesso em linha: | https://www.mdpi.com/2076-3417/11/7/3288 |
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